Feasibility study of direct flow gas core reactor system
Direct flow gas core nuclear reactor propulsion system
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Direct flow gas core nuclear reactor propulsion system
Positionable despun thermal shield to control temperature and power of solar array for spacecraft on-board power during 0.2 AU Pioneer space probe
Teflon and high density phenolic-nylon models evaluated at various enthalpies and heating rates under supersonic conditions
Mathematical design parameter analysis for ultraviolet density sensor calibration fixture
Gravity gradient stabilized, lenticular satellite for passive communications
Reduction of thermal deflections and control of temperature distribution in parts of Advanced Orbiting Solar Observatory /AOSO/
Low thrust rotary and percussive drills for sampling lunar surface
Algorithm formulation for evaluation of strapping arrangement programs for PAM multimode commutation system of Saturn telemetry system
Insulation system for solid propellant rocket engine
Turboprop, fan-in-wing, and propulsive wing concepts for V/STOL commercical transport aircraft
Thin film oxygen partial pressure sensor
Advanced space environmental effects sensor using active control of sensor temperature
Design of fluid line connectors depending solely upon cold forming of metal to carry structural loads and to make helium leak-tight seal
Mobility and structural analyses of bellows concept for lunar roving vehicle
Magnetic-sector mass spectrometer for Mars atmosphere analysis
Poison control tube and manifold system for reactivity control of tungsten water moderated rocket reactor
Freeze-out technique for control of trace contaminants within manned spacecraft atmospheres
Method for physical recovery of carbon dioxide from space cabin atmosphere and chemical recovery of metabolic oxygen